NZ199359A - Lead/rubber spiral element for earthquake damper - Google Patents
Lead/rubber spiral element for earthquake damperInfo
- Publication number
- NZ199359A NZ199359A NZ199359A NZ19935981A NZ199359A NZ 199359 A NZ199359 A NZ 199359A NZ 199359 A NZ199359 A NZ 199359A NZ 19935981 A NZ19935981 A NZ 19935981A NZ 199359 A NZ199359 A NZ 199359A
- Authority
- NZ
- New Zealand
- Prior art keywords
- damper element
- damper
- sheet
- vibration
- lead
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
- F16F1/371—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by inserts or auxiliary extension or exterior elements, e.g. for rigidification
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
- F16F1/42—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing
- F16F1/50—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by the mode of stressing loaded mainly in shear
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2236/00—Mode of stressing of basic spring or damper elements or devices incorporating such elements
- F16F2236/10—Shear
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Health & Medical Sciences (AREA)
- Child & Adolescent Psychology (AREA)
- Vibration Prevention Devices (AREA)
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
- Vibration Dampers (AREA)
Description
t 99359
Priority Dsts(s): .
Cpmg&e'ia Spocsfication FHed: 7SL&& tOME>\ |42>] £02-0^)02 j Fibr-jJiZ. Class:
Publication Date: , ...2A.AUS.m P.O. Joyrnsi IMo: .. r?-bl j
_J
Patents Form No.5
NEW ZEALAND
PATENTS ACT 19 53
COMPLETE SPECIFICATION "DAMPER ELEMENT"
i-jWE NIPPON KOKAN KABUSHIKI KAISHA, a Japanese corporation, of 1-2, 1-chome, Maruouchi, Chiyoda-Tokyo, Japan,
hereby declare the invention, for which -I-/we pray that a patent may be granted to me/us,,and the method by which it is to be performed, to be particularly described in and by the following statement:-
ffoJIowed by page I A.)
1 Q C 7 r; O I s S J J 7
- 1A -
This invention relates to a damper element as used to suppress the vibration of a structure resulting from the occurence of earthquake, to a smaller extent.
The conventional damper element of this type 5 includes:
(1) an oil damper element utilizing the viscosity of oil and
(2) a viscoelastic damper element utilizing the high viscosity of a high-polymeric material.
In the oil damper element, the viscosity of oil varies with a variation of a temperature prevalent in an installation site, varying a damper performance. Furthermore, the oil suffers oxidation during the use,
thus requiring a periodical oil replacement and main-15 tenance. The viscoelastic damper element has a higher temperature dependence due to a variation in temperature prevalent in the installation site. It is therefore difficult to obtain a high performance throughout the year. Moreover, there is a risk that the viscoelastic 20 damper element will be deteriorated where the circumstances of the installation site are worse.
It is accordingly the object of this invention to provide a maintenance-free damper element having a smaller temperature dependence.
According to this invention there is provided a
\
damper element comprising a lead sheet and a high polymeric material sheet spirally and alternately wound
1 o Q - R Q
I s S J /
spiral, circular configuration with these sheets bonded to each other and with the alternate sheet layers stacked one upon the other in a radial direction of the circular configuration.
This invention can be more fully understood from 10 the following detailed description when taken in conjunction with the accompanying drawings, in which:
Fig. 1 is a perspective view showing a damper element according to one embodiment of this invention;
Fig.2 is a cross-sectional view showing a test 15 piece;
Fig.3 is an explanatory view showing the hysteresis loop of the test piece;
Fig.4 is a longitudinal cross-sectional view showing one form of a damper device with a damper incor-20 porated therein;
Fig. 5 is a transverse cross-sectional view as taken along line V - V in Fig. 4; and
Fig. 6 is an explanatory view showing the Fig. 4 damper device as applied to a spherical tank. 25 One embodiment of a damper element according to this invention will be explained below by referring to Fig. 1.
A band-like lead sheet 1 and vibration-proof rubber sheet 2 as a vibration-proof sheet are spirally and intimately wound to provide a damper element of a spiral configuration with the alternate layers of the sheet 1 and vibration-proof sheet 2 alternately stacked one upon the other in a radial direction. A shearing energy acting on one and the other surfaces of the spiral configuration is absorbed by the deformation of the lead sheet and vibration-proof sheet.
Now the formation of the test piece of the damper element will be explained below.
The test piece of the damper element is obtained by spirally and intimately winding a 50 mm wide x 2 mm thick lead sheet 1 and 50 mm wide x 2 mm thick vibration-proof rubber sheet (vibration-proof sheet) 2 by a take-up machine to provide a spiral, circular configuration. In order to readily retain the circular spiral configuration of the lead sheet 1 and vibration-proof sheet 2 when a shearing load acts upon the spiral configuration, a vibration-proof rubber layer is attached as a hoop member 4 to the outer periphery of the spiral configuration with a hoop tension added thereto. The resultant damper element 3 has an inner diameter d of 90 rnm and outer diameter D of 280 mm. As a material of the vibration-proof rubber sheet use is made of a butyl series with a rubber hardness of Hs 50 (JIS). A pair of holding plates 5, 5 with an annular projection 5a are
1 9
4
baked to be each attached to the upper and lower surfaces of the damper element 3 with the damper element 3 fitted inside the annular projections 5a, 5a of the holding plates 5, 5. In this way, the test piece is manufactured with the lead sheet 1 and vibration-proof sheet 2 intimately contacted with each other and with the vibration-proof sheet 2 and the holding plate 5, 5 intimately contacted with each other.
A shearing load is applied at a frequency of 1 to 4 Hz to the test piece, obtaining a stabilized hysteresis as shown in Fig. 3. Since an energy corresponding to an area W as enclosed by the hysteresis loop is applied to the lead sheet 1 and vibration-proof sheet 2 to cause it to be absorbed therein, vibrations of a structure can be effectively suppressed. In this case, the value of a loss tangent 3 showing an energy absorption capability is around 1.0 and it is possible to obtain an effect equal to, or greater than, that of a conventional viscoelastic damper element. Note, however, that
K2
Kl where
*2
W
199359
= Pmax/6max
Since the temperature dependence of the lead sheet 1, one of the constituent elements of the damper element 3, is smaller, a relatively stabilized, high performance can be secured even if a temperature prevalent at the 5 installation site varies. Thus, the constituent members of the damper element hardly suffer deterioration and is manitenance-free.
A damper element-equipped damper device as applied to a spherical tank will be explained below be referring 10 to Figs. 4 to 6.
A vibration proof rubber layer is disposed as a hoop member around the spiral configuration of a damper element and a pair of upper and lower holding plates 11, 11 each having radially inner and outer annular projec-15 tions 11a, 11a are baked to the upper and lower surfaces of the damper element 3 respectively. In Fig. 4, reference numeral 12 shows a cylindrical casing having a fixed flange 12a at its lower end. In the rear surface of the top plate of the casing are provided annular 20 recesses into which the corresponding annular projections of one of the holding plates 11, 11 are fitted. In the central portion of the top plate of the casing is mounted an upper spherical bearing 14 with a bore through which a rocking shaft 13 extends. A spherical 25 slide plate 15 is fitted into a spacing defined between the annular projections 11a, 11a of -the lower holding
199359
plate 11. In the central hole of the spherical slide plate 15 is disposed a lower spherical bearing 16 with a bore through which the rocking shaft 13 extends. Thus, the shaft 13 extends through the bores of the upper and 5 lower spherical bearings 14, 16 and the upper end of the shaft 13 is connected by a pin to a rod 17 which in turn is mounted on the lower portion of a spherical tank T. The displacement of the spherical tank T permits a lateral movement of the slide plate 15. A friction plate 10 18 is placed between the slide plate 15 and a bottom plate of the casing 12 to permit the ready lateral movement of the slide plate 15. A plurality of damper devices so constructed are secured by anchor bolts 19 on the circluar portion of a foundation for the spherical 15 tank T as shown in Fig. 6 and the upper ends of the rocking shafts 13 are connected by the corresponding pins to the corresponding rods 17, ... which are mounted on the lower section of the spherical tank T.
Now suppose that the spherical tank T is displaced 20 due to the occurrence of earthquake. In this case, the displacement of the spherical tank T is transmitted through the rod 17 to the damper device 20. That is, the rocking shaft 13 connected to the rod 17 is rocked with the spherical bearing 14 and a fulcrum, causing 25 the slide plate 15 to be moved laterally to impart a shearing force to the damper element 3. Since the shearing energy resulting from the occurrence of
€)
earthquake is absorbed by the damper element 3, it is possible to suppress the vibration of the spherical tank T to a smaller extent. Note that, if the damping constant of the structure is smaller, it is possible to 5 effectively suppress the vibration of the structure.
The.damper element may be formed in a circular configuration by alternately fitting one of annular lead sheets of varying diameters into the other of annular vibration-proof rubber sheets of varying diameters. A 10 lead sheet and vibration-proof sheet may be spirally and intimately wound to provide a damper element of a spiral configuration with the spirally stacked layers adhesively bonded to each other, and the resultant damper ele^-ment may be compression-bonded directly between the mem-15 bers of the structure, without interposing any holding plates, which suffers' a possible relative displacement resulting from the occurrence of earthquake. If, in this case, the outer periphery of the damper element is firmly encircled by a vibration-proof rubber layer (as a 20 hoop member) the intimately bonded state between the lead sheet and vibration-proof sheet is effectively maintained when the shearing load acts on the damper element. ' With the holding plates each bonded to the upper and lower surfaces of the damper element the 25 structure can be readily mounted on the installation site and exhibit a stabilized performance. Instead of bonding the holding plates to the damper element,
1 o o
I / /
piercing projections may be provided on the -inner side surfaces of the holding plates and the damper element may be incorporated into the damper device with a pair of holding plates each compressed to the upper and lower surfaces of the circular configuration while the piercing projections are pierced into the damper element, whereby the movement of the holding plates i:s transmitted to the vibration-proof sheet.
With the damper element of this invention, a possible displacement of the structure resulting from the occurence of earthquake can be suppressed to a smaller extent. Because the lead plate, one of the constituent elements of the damper element, has a smaller temperature dependence, the damper can maintain a relatively stable, high performance, even if a temperature prevalent at the installation site varies. The constituent elements of the damper element are hardly deteriorated, thus requiring no maintenance.
Claims (4)
1. A damper element comprising a lead sheet and a high polymeric material sheet spirally and alternately wound to provide a spiral, circular configuration with these 5 sheets bonded to each other and with said alternate layers of the circular configuration stacked one upon the other in a radial direction of the circular configuration. 10
2. A damper element according to claim 1, in which said spiral, circular configuration has a hoop of high polymeric.material provided on the outer periphery thereof.
3. A damper element according to claim 1 or 2, in which two holding plates are attached one to the 15 upper and one to the lower surfaces of said spiral, circular configuration through said high polymeric material sheet.
4. A damper element, substantially as hereinbefore described with reference to the accompanying drawings. ATTORNEYS FOR THE APPLICANTS 2*APR198£
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP56021888A JPS57137739A (en) | 1981-02-17 | 1981-02-17 | Aseismatic metallic damper |
Publications (1)
Publication Number | Publication Date |
---|---|
NZ199359A true NZ199359A (en) | 1984-08-24 |
Family
ID=12067640
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NZ199359A NZ199359A (en) | 1981-02-17 | 1981-12-22 | Lead/rubber spiral element for earthquake damper |
Country Status (5)
Country | Link |
---|---|
US (1) | US4483426A (en) |
JP (1) | JPS57137739A (en) |
CA (1) | CA1181441A (en) |
NZ (1) | NZ199359A (en) |
PT (1) | PT74241A (en) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4899323A (en) * | 1986-08-04 | 1990-02-06 | Bridgestone Corporation | Anti-seismic device |
JP2589727B2 (en) * | 1988-01-26 | 1997-03-12 | 株式会社ブリヂストン | Seismic isolation rubber |
FR2634164B1 (en) * | 1988-07-12 | 1994-03-04 | Application Machines Motrices | ELASTIC SUSPENSION DEVICE AND LOAD DAMPING, PARTICULARLY FOR VEHICLE |
JP2895268B2 (en) * | 1990-08-13 | 1999-05-24 | オイレス工業株式会社 | Plastic energy absorber |
US5390904A (en) * | 1993-10-08 | 1995-02-21 | Illinois Tool Works, Inc. | Attenuated hinge spring assembly |
US5842312A (en) * | 1995-03-01 | 1998-12-01 | E*Sorb Systems | Hysteretic damping apparati and methods |
JP2003043862A (en) * | 2001-05-23 | 2003-02-14 | Ricoh Co Ltd | Latent image carrier, image forming device, and vibration damping member |
JP4366935B2 (en) | 2002-01-16 | 2009-11-18 | オイレス工業株式会社 | Friction damper |
KR100507645B1 (en) * | 2002-12-11 | 2005-08-10 | 현대자동차주식회사 | Device for blocking the noise from engine of car |
US20040123530A1 (en) * | 2002-12-30 | 2004-07-01 | Luis Dorfmann | Seismic and vibration isolation system |
US7258287B2 (en) * | 2004-06-03 | 2007-08-21 | Siemens Vdo Automotive Corporation | Modular fuel injector with a spiral damper member and method of reducing noise |
US20060169557A1 (en) * | 2005-02-01 | 2006-08-03 | Material Sciences Corporation | Constrained layer viscoelastic laminate tuned mass damper and method of use |
CN103790253A (en) * | 2012-10-31 | 2014-05-14 | 沈阳建筑大学 | Steel lead lamination node damper |
DE102016212454A1 (en) * | 2016-07-08 | 2018-01-11 | Bayerische Motoren Werke Aktiengesellschaft | Storage of a device exposed to a noise source in a motor vehicle |
US10677312B2 (en) | 2018-02-15 | 2020-06-09 | General Electric Company | Friction shaft damper for axial vibration mode |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE509562C (en) * | 1930-10-10 | Adolf Donecker | Cushioning, especially for cars | |
US1574985A (en) * | 1924-07-02 | 1926-03-02 | Eugene E Mcwain | Mounting for vibrating machines |
GB362470A (en) * | 1930-07-29 | 1931-11-30 | Leopold Rado | Underlay for machines |
US2176971A (en) * | 1937-04-01 | 1939-10-24 | Briggs Mfg Co | Land vehicle |
US2932503A (en) * | 1956-08-28 | 1960-04-12 | American Machine & Metals | Springs |
US3263954A (en) * | 1963-11-15 | 1966-08-02 | Korfund Dynamics Corp | All-directional shock mount |
-
1981
- 1981-02-17 JP JP56021888A patent/JPS57137739A/en active Granted
- 1981-12-22 NZ NZ199359A patent/NZ199359A/en unknown
-
1982
- 1982-01-04 CA CA000393510A patent/CA1181441A/en not_active Expired
- 1982-01-05 PT PT74241A patent/PT74241A/en not_active IP Right Cessation
-
1984
- 1984-04-27 US US06/604,402 patent/US4483426A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
JPS6216336B2 (en) | 1987-04-11 |
US4483426A (en) | 1984-11-20 |
PT74241A (en) | 1982-02-01 |
JPS57137739A (en) | 1982-08-25 |
CA1181441A (en) | 1985-01-22 |
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